AD/IAI-W/25 - Pressurisation System - Emergency Operating Procedures (Cth)
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
Israel Aircraft Industries 1123 and 1124 (Westwind) Series Aeroplanes
AD/IAI-W/25 Pressurisation S ystem - Emergency Operating
Procedures
10/2002
DM
Applicability: Model 1124 and 1124A aeroplanes.
Requirement: Unless already accomplished, insert the following temporary revisions (T/R) into the appropriate Aircraft Flight Manual (AFM):
Aeroplane Model AFM T/R Number/Date
1124 No. 3 dated 16 January 2001
1124A No. 5 dated 16 January 2001
Note: CAA Israel AD 21-02-07-01 refers.
Compliance: Before 20 September 2002.
This Airworthiness Directive becomes effective on 28 August 2002.
Background: This Directive requires the amendment of the AFM introducing revised emergency operating procedures when a warning of excessive cabin altitude is activated.
James Coyne
Delegate of the Civil Aviation Safety Authority 19 August 2002
The above AD is notified in the Commonwealth of Australia Gazette on 28 August 2002.
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